Please use this identifier to cite or link to this item: http://hdl.handle.net/10603/532795
Title: Numerical simulation and analysis of cavitating Flow around hydrofoil and in injector nozzle
Researcher: Singh, Srijna
Guide(s): Danish, Mohammad and Saha, Kaushik
Keywords: Engineering
Engineering and Technology
Engineering Mechanical
University: Bennett University
Completed Date: 2023
Abstract: Cavitation occurs in flow regions where the hydrodynamic effect reduces the local pressure newlinebelow the saturation vapor pressure of the liquid, causing the formation of vapor bubbles. When newlinethese vapor bubbles enter the region of higher pressure, they collapse violently producing newlineenough force to damage the solid body. In case of hydrofoils, cavitation can affect the newlinehydrodynamic and structural performance potentially. In injector nozzles, cavitation can cause newlinea fuel injection instability and decreased fuel efficiency. Cavitation on hydrofoils and nozzles newlinemainly depends on the flow parameters, shape and material of the hydrofoil or nozzle. In the newlinepresent work to study the cavitation phenomenon three different studies have been made on newlinehydrofoils and in injector nozzle. In first part of the work, the performance of two different newlinecavitation model and four different turbulence models is compared with the available newlineexperimental data on cavitating NACA4412 and Clark-y hydrofoil in terms of lift coefficient, newlinedrag coefficient, Strouhal number and velocity profiles using ANSYS Fluent. Among all the newlineturbulence models, the Realizable k-and#120598; turbulence was found to be more accurate, whereas the newlineZwart-Gerber-Belamri cavitation model is found to be more reliable. Using the Realizable k-and#120598; newlineand Zwart-Gerber-Belamri cavitation model, the research was further extended to study the newlinehydrodynamic and structural performance of 3D stainless steel MHKF-180 and NACA4418 newlinecavitating hydrofoils using one-way fluid structure interaction (FSI). The simulation is newlineperformed at a chord-based Reynolds number, Re = 750000, for different cavitation numbers newlineand angles of attack. On comparing the hydrodynamic performance of both the foils, in terms newlineof lift coefficient, MHKF-180 found to perform better than NACA4418 under the cavitating newlinecondition. Whereas, from structural point of view, the MHKF-180 shows larger tip deformation newlineand von Mises stress than NACA4418 hydrofoil. Further, in the last part of the work, the newlinenumerical investigat
Pagination: xvii; 108p.
URI: http://hdl.handle.net/10603/532795
Appears in Departments:Department of Mechanical and Aerospace Engineering

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01_title.pdf.pdfAttached File45.12 kBAdobe PDFView/Open
02_prelim pages.pdf.pdf755.57 kBAdobe PDFView/Open
03_content.pdf.pdf229.75 kBAdobe PDFView/Open
04_abstract.pdf.pdf193.27 kBAdobe PDFView/Open
05_chapter 1.pdf.pdf572.06 kBAdobe PDFView/Open
06_chapter 2.pdf.pdf275.43 kBAdobe PDFView/Open
07_chapter 3.pdf.pdf883.69 kBAdobe PDFView/Open
08_chapter 4.pdf.pdf1.44 MBAdobe PDFView/Open
09_chapter 5.pdf.pdf1.48 MBAdobe PDFView/Open
10_chapter 6.pdf.pdf664.43 kBAdobe PDFView/Open
11_chapter 7.pdf.pdf254.52 kBAdobe PDFView/Open
12_annexures.pdf.pdf386.75 kBAdobe PDFView/Open
80_recommendation.pdf297.29 kBAdobe PDFView/Open
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